CN115683538A - Wind tunnel dust environment simulation device and method based on plasma excitation - Google Patents
Wind tunnel dust environment simulation device and method based on plasma excitation Download PDFInfo
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Abstract
The invention discloses a wind tunnel dust environment simulation device and method based on plasma excitation, wherein the device comprises a dust generation assembly and a wind tunnel generation array which are arranged at an inlet of a wind tunnel experiment section; the sand and dust generating assembly is used for injecting falling sand into the wind tunnel; the wind field generation array is formed by arranging a plurality of plasma excitation assemblies in an array manner; the plasma excitation assembly is used for periodically and alternately generating vertical rising jet flow and rotary flow, and the falling sand injected by the sand and dust generation assembly forms a required sand and dust environment under the coupling action of the flow in two directions and the flow in the wind tunnel. The invention generates plasma by ionizing air, charged particles collide with each other or neutral particles under the action of an electric field/magnetic field, and jet flow is induced to be generated, so that vertical speed and rotating speed are provided for sand and dust, and the running track of the sand and dust in a real environment is simulated.
Description
Technical Field
The invention belongs to the technical field of wind tunnel experiments, and particularly relates to a wind tunnel sand and dust environment simulation device and method based on plasma excitation.
Background
The area occupied by the gobi in the desert is wide, the sand and dust weather is numerous, and the influence area is large. When the aircraft works in a sand environment, the structural performances of an engine, wings and the like of the aircraft are greatly influenced, and even safety accidents can be caused under severe conditions; with the wide application of wind power generation technology, sand storm and other sand weather can also affect the performance and safety of wind turbines, and relevant research is gradually paid attention.
At present, the research on the sand and dust environment such as sand storm is carried out, and besides the research on the field, the research needs to be completed by simulating the sand and dust environment through a wind tunnel experiment. The current common wind sand simulation system mostly adopts the modes of ground sand paving and vertical sand falling. If ground sand paving is adopted, the wind sand flow is mainly limited within 200mm of the ground, the wind sand is difficult to be uniformly distributed on the whole wind tunnel section, the effective area is small, and only small-size low experimental model research can be carried out; the same problem exists in vertical sand falling, under the condition that the wind speed is not high enough, sand and dust can settle rapidly, the distribution is uneven when the sand and dust reaches the experimental section, in addition, only the wind and sand flow with single speed can be simulated, the movement direction of the sand and dust in nature, particularly the movement direction of the sand and dust in sand storm weather, is complex, and the existing method can not truly simulate the sand and dust environment.
Disclosure of Invention
The invention provides a wind tunnel sand-dust environment simulation device and method based on plasma excitation, aiming at solving the problem that the existing sand-dust environment simulation technology cannot truly simulate a sand-dust environment. The invention generates plasma by ionizing air, charged particles collide with each other or neutral particles under the action of an electric field/magnetic field, and then jet flow is induced to be generated, so that vertical speed and rotating speed are provided for sand and dust, and the running track of the sand and dust in a real environment is simulated.
The invention is realized by the following technical scheme:
a wind tunnel dust environment simulation device based on plasma excitation comprises a dust generation assembly and a wind field generation array, wherein the dust generation assembly and the wind field generation array are arranged at an inlet of a wind tunnel experiment section;
the sand and dust generating assembly is used for injecting falling sand into the wind tunnel;
the wind field generation array is formed by arraying a plurality of plasma excitation assemblies;
the plasma excitation assembly is used for periodically and alternately generating vertical rising jet flow and rotating flow;
and the falling sand injected by the sand and dust generating assembly forms a required sand and dust environment under the coupling action of the flow in two directions and the flow in the wind tunnel.
As a preferred embodiment, the plasma excitation assembly of the present invention includes a magnetic field generating unit, a vertical rising jet generating unit, and a rotational flow generating unit;
the vertical rising jet flow generating unit comprises an annular alternating current high-voltage electrode and an annular alternating current low-voltage electrode, and is powered by an alternating current power supply;
the rotary flow generating unit comprises an annular direct current high-voltage electrode and an annular direct current low-voltage electrode, and is powered by a direct current power supply; the annular direct current high-voltage electrode and the annular direct current low-voltage electrode are coaxially arranged, the annular direct current low-voltage electrode is arranged on the outer side of the annular direct current high-voltage electrode, and the magnetic field generating unit is arranged below the rotary flow generating unit.
As a preferred embodiment, the magnetic field generating unit of the present invention employs a toroidal magnetic field generating device;
the outer diameter of the annular direct-current high-voltage electrode is equal to the inner diameter of the annular magnetic field generating device;
the inner diameter of the annular direct current low-voltage electrode is equal to the outer diameter of the annular magnetic field generating device.
In a preferred embodiment, the electrodes in the swirling flow generating unit and the vertical rising jet generating unit of the present invention are both made of copper foil.
As a preferred embodiment, the plasma excitation assembly of the present invention further comprises a function generator and a voltage regulator;
the function generator is used for respectively controlling the periodic work and the closing of the magnetic field generating unit, the vertical rising jet flow generating unit and the rotary flow generating unit;
and the voltage regulator is used for regulating the amplitude and the frequency of the input voltage of the vertical rising jet flow generating unit and the rotary flow generating unit.
In a preferred embodiment, the function generator of the present invention is controlled by outputting a drive signal in a plurality of channels.
As a preferred embodiment, the voltage regulator of the present invention includes a dc voltage regulator and an ac voltage regulator;
the direct current voltage regulator is connected with the direct current power supply, and the alternating current voltage regulator is connected with the alternating current power supply.
In a second aspect, the present invention provides a working method of the wind tunnel dust environment simulation apparatus, including:
operating the wind tunnel to generate uniform incoming flow;
initializing a function generator, wherein the function generator respectively outputs driving signals to the magnetic field generating unit, the vertical rising jet generating unit and the rotary flow generating unit;
controlling the magnetic field generating unit and the rotation generating unit to be started simultaneously, and controlling the vertical rising jet flow generating unit to be closed to generate rotary flow;
after a preset time interval, controlling the vertical rising jet flow generating unit to be started, and controlling the magnetic field generating unit and the rotary flow generating unit to be closed to generate vertical rising jet flow;
periodically and alternately generating rotary flow and vertical rising jet flow at preset time intervals, wherein the flow in two directions is coupled with the flow in the wind tunnel, so that a required wind field structure is formed;
and opening the sand and dust generating assembly, injecting falling sand into the wind tunnel, and forming a required sand and dust environment under the action of the wind field structure.
As a preferred embodiment, the initialization function generator of the present invention specifically comprises:
setting output signals of a function generator, wherein 3 output channels of the function generator synchronously output 5V TTL signals, and the potential difference and the frequency of the signals output by the 3 output channels are consistent;
the waveform phases of the signals input into the magnetic field generating unit and the rotating flow generating unit are consistent;
the phase difference between the signal input into the vertical rising jet flow generating unit and the signal waveform input into the magnetic field generating unit and the rotating flow generating unit is 0.5T, wherein T is a signal period.
As a preferred embodiment, the method of the present invention further comprises:
and adjusting the intensity of the formed dust by adjusting the amplitude and frequency of the input voltage of the vertical rising jet flow generating unit and the input voltage of the rotating flow generating unit.
The invention has the following advantages and beneficial effects:
the invention adopts a pure electric driving mode, plasma is generated by ionizing air, then charged particles collide with each other or neutral particles under the action of an electric field/magnetic field, jet flow is induced to be generated, vertical speed and rotating speed are provided for sand and dust, and the running track of the sand and dust in a real environment is simulated.
According to the invention, the control of the vertical wind speed and the rotating wind speed is realized by controlling the electromagnetic field intensity and the charged ion density, so that the sand dust is prevented from falling due to gravity before reaching the experimental section, and the distribution uniformity of the sand dust in the experimental section is improved.
The invention has simple structure, convenient maintenance, low cost and easy realization.
Drawings
The accompanying drawings, which are included to provide a further understanding of the embodiments of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the principles of the invention. In the drawings:
fig. 1 is a schematic structural diagram of an apparatus according to an embodiment of the present invention.
Fig. 2 is a schematic structural diagram of a plasma excitation assembly according to an embodiment of the present invention.
Fig. 3 is a sectional view of a plasma excitation unit according to an embodiment of the present invention.
Fig. 4 is a top view of a plasma excitation unit according to an embodiment of the present invention.
Fig. 5 is a bottom view of the plasma excitation unit according to the embodiment of the present invention.
FIG. 6 is a schematic diagram of the rotational flow generation of an embodiment of the present invention.
FIG. 7 is a schematic view of vertical jet generation according to an embodiment of the present invention.
Reference numbers and corresponding part names in the drawings:
the magnetic field generating device comprises a wind tunnel 1, a dust generating assembly 2, a wind field generating array 3, a first electrode 4, a second electrode 5, a first insulating medium layer 6, a third electrode 7, an insulating filling layer 8, a second insulating medium layer 9 and a magnetic field generating unit 10.
Detailed Description
Hereinafter, the term "comprising" or "may include" used in various embodiments of the present invention indicates the presence of the invented function, operation or element, and does not limit the addition of one or more functions, operations or elements. Furthermore, as used in various embodiments of the present invention, the terms "comprises," "comprising," "includes," "including," "has," "having" and their derivatives are intended to mean that the specified features, numbers, steps, operations, elements, components, or combinations of the foregoing, are only meant to indicate that a particular feature, number, step, operation, element, component, or combination of the foregoing, and should not be construed as first excluding the existence of, or adding to the possibility of, one or more other features, numbers, steps, operations, elements, components, or combinations of the foregoing.
In various embodiments of the invention, the expression "or" at least one of a or/and B "includes any or all combinations of the words listed simultaneously. For example, the expression "a or B" or "at least one of a or/and B" may include a, may include B, or may include both a and B.
Expressions (such as "first", "second", and the like) used in various embodiments of the present invention may modify various constituent elements in various embodiments, but may not limit the respective constituent elements. For example, the above description does not limit the order and/or importance of the elements described. The foregoing description is for the purpose of distinguishing one element from another. For example, the first user device and the second user device indicate different user devices, although both are user devices. For example, a first element could be termed a second element, and, similarly, a second element could be termed a first element, without departing from the scope of various embodiments of the present invention.
It should be noted that: if it is described that one constituent element is "connected" to another constituent element, the first constituent element may be directly connected to the second constituent element, and a third constituent element may be "connected" between the first constituent element and the second constituent element. In contrast, when one constituent element is "directly connected" to another constituent element, it is understood that there is no third constituent element between the first constituent element and the second constituent element.
The terminology used in the various embodiments of the invention is for the purpose of describing particular embodiments only and is not intended to be limiting of the various embodiments of the invention. As used herein, the singular forms are intended to include the plural forms as well, unless the context clearly indicates otherwise. Unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which various embodiments of the present invention belong. The terms (such as those defined in commonly used dictionaries) should be interpreted as having a meaning that is consistent with their contextual meaning in the relevant art and will not be interpreted in an idealized or overly formal sense unless expressly so defined herein in various embodiments of the present invention.
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is further described in detail below with reference to examples and accompanying drawings, and the exemplary embodiments and descriptions thereof are only used for explaining the present invention and are not meant to limit the present invention.
Examples
Aiming at the problem that the existing wind and sand simulation technology cannot truly simulate a sand and dust environment, the embodiment provides a wind tunnel sand and dust environment simulation device based on plasma excitation.
Specifically, as shown in fig. 1, the device according to the embodiment of the present invention includes a dust and sand generating assembly 2 and a wind field generating array 3, which are disposed at an inlet of an experimental section of a wind tunnel 1. The sand and dust generating assembly 2 is arranged at a position close to the top of the wind tunnel 1, and the wind field generating array 3 is arranged at a position close to the bottom of the wind tunnel 1. The sand and dust generating assembly 2 is used for injecting falling sand into a wind tunnel, and the wind field generating array 3 is formed by arranging a plurality of plasma exciting assemblies in an array mode and used for providing vertical wind speed and rotating wind speed for the sand and dust generated by the sand and dust generating assembly 2, and preventing the sand and dust from falling due to gravity before the sand and dust reaches an experimental section, so that the running track of the sand and dust in a real environment is simulated.
As shown in fig. 2 to 5 in detail, the plasma excitation assembly according to the embodiment of the present invention mainly includes a magnetic field generating unit 10, a plasma generating unit, and the like.
The plasma generating unit is composed of a first electrode 4, a second electrode 5, a third electrode 7 and an insulating medium layer.
The first insulating medium layer 6, the insulating filling layer 8 and the second insulating medium layer are sequentially arranged from top to bottom, the first electrode 4 and the second electrode 5 are both arranged on the upper surface of the first insulating medium layer 6, the second electrode 5 is arranged on the periphery of the first electrode 4, and the third electrode 7 is arranged in the insulating filling layer 8 and is positioned in a gap between the first electrode 4 and the second electrode 5; the magnetic field generating unit 10 is disposed on the lower surface of the second insulating medium layer.
The first electrode 4, the second electrode 5 and the third electrode 7 are all annular electrodes, the third electrode 7 and the first electrode 1 form a vertical rising jet flow generation unit, the first electrode 4 and the second electrode 5 form a rotary flow generation unit, and the two units jointly form a plasma generation unit. Under the working mode of the direct-current power supply, the first electrode 4 is used as a direct-current high-voltage electrode to be connected with a high-voltage output end of the direct-current power supply, and the second electrode 5 is used as a direct-current low-voltage electrode; in the working mode of the alternating current power supply, the third electrode 7 is used as an alternating current high-voltage electrode to be connected with a high-voltage output end of the alternating current power supply, and the first electrode 4 is used as an alternating current low-voltage electrode.
The magnetic field generating unit 10 adopts a ring-shaped magnetic field generating device, and can generate an electromagnetic field with corresponding strength after being electrified.
The outer diameter of the first electrode 4 is equal to the inner diameter of the annular magnetic field generating device, the inner diameter of the second electrode 5 is equal to the outer diameter of the annular magnetic field generating device, and the annular thickness of the third electrode 7 is equal to the annular thickness of the annular magnetic field generating device.
In this embodiment, the first electrode 4, the second electrode 5, and the third electrode 7 are made of copper foil.
In this embodiment, the first insulating dielectric layer 6, the insulating filling layer 8, and the second insulating dielectric layer 9 are made of teflon or polyimide.
The working principle of the device provided by the embodiment of the invention is as follows:
the plasma excitation assembly is used as an active flow control device, high voltage is applied between two electrodes of the plasma generation unit, ionization is carried out between the electrodes or surface air to generate plasma, the charged plasma directionally moves under the action of electric field force, and neutral air is wrapped by collision to generate jet flow. For the vertical rising jet flow generation unit, by applying alternating high voltage, the induced directional motion can be directed to the center of the annular structure, and then a synthetic jet flow which vertically faces upwards is generated. For the rotary flow generating unit, the annular magnetic field generating device is positioned below the first electrode, when the rotary flow generating unit is electrified, gas between the two electrodes can be broken down to form plasma, and the annular magnetic field generating device provides Lorentz force required for driving flow.
The plasma excitation assembly of the embodiment of the invention further comprises a function generator and a voltage regulator.
The function generator can output driving signals in multiple channels, respectively control the work and the closing of the magnetic field generating unit and the plasma generating unit, and can form a sand-dust environment flow field structure together with the wind tunnel incoming flow by alternately generating vertical rising jet flow and rotary flow and the mutual coupling action of the two flows.
The voltage regulator comprises a direct current voltage regulator and an alternating current voltage regulator, and is connected with a direct current power supply or an alternating current power supply and used for supplying power and regulating input parameters such as voltage, frequency and the like. According to the embodiment of the invention, the amplitude and the frequency of the voltage can be adjusted according to actual requirements, and the adjustment of the vertical rising jet flow strength and the rotating flow strength can be respectively realized, namely, the vertical wind speed and the rotating wind speed are regulated and controlled by controlling the electromagnetic field strength and the charged ion density, the falling of sand dust due to gravity is prevented before the sand dust reaches the experimental section, the sand dust distribution uniformity of the experimental section is improved, and the vertical speed and the rotating speed are provided for the sand dust at the same time so as to simulate the wind and sand environments such as a sand storm and the like in the real environment, thereby carrying out the performance test and the characteristic research of an aircraft in the wind and sand environment, and simultaneously, the stress and damage research of a wind turbine and a building can be developed.
The working process of the device provided by the embodiment of the invention comprises the following steps:
step 1, operating the wind tunnel to generate uniform incoming flow.
And step 2, initializing the function generator. Specifically, output signals of a function generator are set, 5V TTL signals are used as output signals for adjusting the channel 1, the channel 2 and the channel 3 synchronously, the potential difference and the frequency of the output signals of the 3 channels are consistent, wherein the waveform phases of the output signals of the channel 1 and the channel 2 are also consistent, the difference between the waveform phase of the channel 3 and the waveform phases of the channel 1 and the channel 2 is 0.5T, and then the function generator is started to output the signals; wherein T is the signal period.
And 3, the output ends of the direct current voltage regulator and the alternating current voltage regulator are respectively connected with the input ends of the direct current power supply and the alternating current power supply, so that the output voltage of the direct current power supply and the output voltage and frequency of the alternating current power supply can be regulated.
And 4, respectively connecting 3 output ends of the function generator with a high-voltage alternating current power supply of the magnetic field generating unit, a high-voltage alternating current power supply of the vertical rising jet flow generating unit and a high-voltage direct current power supply of the rotary flow generating unit, and respectively controlling the driving modules in the corresponding equipment by the output signals of 3 channels.
And 5, controlling the magnetic field generating unit and the rotary flow generating unit to be started simultaneously by the function generator, closing the vertical rising jet flow generating unit at the moment, and generating rotary flow as shown in figure 6.
After the step 6,0.5T, the vertical rising jet flow generating unit is started, the magnetic field generating unit and the rotational flow generating unit are closed, and the vertical rising jet flow as shown in fig. 7 is generated.
And 7, periodically and alternately performing the step 4 and the step 5 with a phase difference of 0.5T, so that the periodic generation of vertical rising jet flow and rotating flow is realized, and the flow in two directions is coupled with the flow in the wind tunnel to jointly form a sand-dust environment wind field structure.
And 8, opening the sand and dust generating assembly, simulating sand and dust environments such as sand and dust storms and the like, and changing the sand and dust strength by adjusting the pressure regulator.
The above-mentioned embodiments are intended to illustrate the objects, technical solutions and advantages of the present invention in further detail, and it should be understood that the above-mentioned embodiments are merely exemplary embodiments of the present invention, and are not intended to limit the scope of the present invention, and any modifications, equivalent substitutions, improvements and the like made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (10)
1. A wind tunnel dust environment simulation device based on plasma excitation is characterized by comprising a dust generation assembly and a wind field generation array, wherein the dust generation assembly and the wind field generation array are arranged at an inlet of a wind tunnel experiment section;
the sand and dust generating assembly is used for injecting falling sand into the wind tunnel;
the wind field generation array is formed by arranging a plurality of plasma excitation assemblies in an array manner;
the plasma excitation assembly is used for periodically and alternately generating vertical rising jet flow and rotating flow;
and the falling sand injected by the sand and dust generating assembly forms a required sand and dust environment under the coupling action of the flow in two directions and the flow in the wind tunnel.
2. The wind tunnel dust and sand environment simulation device based on plasma excitation according to claim 1, wherein the plasma excitation assembly comprises a magnetic field generation unit, a vertical rising jet flow generation unit and a rotating flow generation unit;
the vertical rising jet flow generating unit comprises an annular alternating current high-voltage electrode and an annular alternating current low-voltage electrode, and is powered by an alternating current power supply;
the rotary flow generating unit comprises an annular direct current high-voltage electrode and an annular direct current low-voltage electrode, and is powered by a direct current power supply; the annular direct current high-voltage electrode and the annular direct current low-voltage electrode are coaxially arranged, the annular direct current low-voltage electrode is arranged on the outer side of the annular direct current high-voltage electrode, and the magnetic field generating unit is arranged below the rotary flow generating unit.
3. The wind tunnel dust and sand environment simulation device based on plasma excitation according to claim 2, wherein the magnetic field generation unit adopts a ring-shaped magnetic field generation device;
the outer diameter of the annular direct-current high-voltage electrode is equal to the inner diameter of the annular magnetic field generating device;
the inner diameter of the annular direct current low-voltage electrode is equal to the outer diameter of the annular magnetic field generating device.
4. The wind tunnel dust environment simulation device based on plasma excitation according to claim 2, wherein the electrodes in the rotating flow generation unit and the vertical rising jet flow generation unit are made of copper foil.
5. The wind tunnel dust and sand environment simulation device based on plasma excitation according to claim 2, wherein the plasma excitation assembly further comprises a function generator and a voltage regulator;
the function generator is used for respectively controlling the periodic work and the closing of the magnetic field generating unit, the vertical rising jet flow generating unit and the rotary flow generating unit;
and the voltage regulator is used for regulating the amplitude and the frequency of the input voltage of the vertical rising jet flow generating unit and the rotary flow generating unit.
6. The wind tunnel dust and sand environment simulation device based on plasma excitation according to claim 5, wherein the function generator is controlled by adopting a multi-channel output driving signal mode.
7. The wind tunnel dust environment simulation device based on plasma excitation according to claim 5, wherein the voltage regulator comprises a direct current voltage regulator and an alternating current voltage regulator;
the direct current voltage regulator is connected with the direct current power supply, and the alternating current voltage regulator is connected with the alternating current power supply.
8. The working method of the wind tunnel dust environment simulation device based on the plasma excitation according to any one of claims 2 to 7, characterized by comprising the following steps:
operating the wind tunnel to generate uniform incoming flow;
initializing a function generator, wherein the function generator respectively outputs driving signals to the magnetic field generating unit, the vertical rising jet generating unit and the rotary flow generating unit;
controlling the magnetic field generating unit and the rotation generating unit to be started simultaneously, and controlling the vertical rising jet flow generating unit to be closed to generate rotary flow;
after a preset time interval, controlling the vertical rising jet flow generating unit to start, and controlling the magnetic field generating unit and the rotary flow generating unit to close to generate vertical rising jet flow;
periodically and alternately generating rotary flow and vertical rising jet flow at preset time intervals, wherein the flow in two directions is coupled with the flow in the wind tunnel, so that a required wind field structure is formed;
and opening the sand and dust generating assembly, injecting falling sand into the wind tunnel, and forming a required sand and dust environment under the action of the wind field structure.
9. The operating method according to claim 8, characterized in that the function generator is initialized, in particular:
setting output signals of a function generator, wherein 3 output channels of the function generator synchronously output 5V TTL signals, and the potential difference and the frequency of the signals output by the 3 output channels are consistent;
the waveform phases of the signals input into the magnetic field generating unit and the rotating flow generating unit are consistent;
the phase difference between the signal input into the vertical rising jet flow generating unit and the signal waveform input into the magnetic field generating unit and the rotating flow generating unit is 0.5T, wherein T is a signal period.
10. The method of operation of claim 8, further comprising:
and adjusting the intensity of the formed dust by adjusting the amplitude and frequency of the input voltage of the vertical rising jet flow generating unit and the input voltage of the rotating flow generating unit.
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Citations (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1326429A (en) * | 1969-10-31 | 1973-08-15 | Siemens Ag | Production of high-velocity gas jets |
| WO2011156413A2 (en) * | 2010-06-07 | 2011-12-15 | University Of Florida Research Foundation, Inc. | Dielectric barrier discharge wind tunnel |
| CN103175672A (en) * | 2013-02-28 | 2013-06-26 | 山东大学 | Construction machinery radiator air tunnel capable of simulating wind and sand impact and using method thereof |
| CN104251767A (en) * | 2013-06-28 | 2014-12-31 | 中国科学院工程热物理研究所 | Gas flow field measurement system based on alternating-current discharge plasma sensors |
| CN105836165A (en) * | 2016-05-05 | 2016-08-10 | 哈尔滨工业大学 | Space environment ground-based simulation plasma generating device and plasma generating method achieved through device |
| CN207623147U (en) * | 2017-12-27 | 2018-07-17 | 天津亭华科技有限公司 | A kind of sand dust test chamber |
| CN109470504A (en) * | 2018-12-13 | 2019-03-15 | 中国航天空气动力技术研究院 | A kind of phase shift device and method for electro-arc heater arc root rotation of strengthening communication |
| CN110082058A (en) * | 2019-04-22 | 2019-08-02 | 南京航空航天大学 | A kind of multi-fan array wind-tunnel that simulating a variety of extreme wind fields and simulation of wind method |
| CN110763966A (en) * | 2019-11-21 | 2020-02-07 | 华北电力大学（保定） | Sand and dust weather simulation experiment system |
| CN110933832A (en) * | 2019-07-16 | 2020-03-27 | 中国人民解放军空军工程大学 | Single power supply driven array type plasma synthetic jet flow control device and flow control method |
| CN211264574U (en) * | 2020-02-03 | 2020-08-14 | 海南泰和鸿鼎实业有限公司 | Sand storm simulator |
| CN111577561A (en) * | 2020-04-24 | 2020-08-25 | 南京理工大学 | Device for improving jet intensity of annular electrode exciter and working method thereof |
| CN112067237A (en) * | 2020-09-24 | 2020-12-11 | 北京卫星环境工程研究所 | Hypersonic wind tunnel based on plasma |
| CN112135408A (en) * | 2020-09-24 | 2020-12-25 | 北京卫星环境工程研究所 | Plasma parameter measuring method for plasma wind tunnel |
| CN112399694A (en) * | 2020-11-04 | 2021-02-23 | 中国空气动力研究与发展中心低速空气动力研究所 | Annular plasma exciter and pneumatic excitation generating method thereof |
| JP2021047086A (en) * | 2019-09-18 | 2021-03-25 | 株式会社Ｓｕｂａｒｕ | Wind tunnel test apparatus |
-
2022
- 2022-11-25 CN CN202211487216.6A patent/CN115683538B/en active Active
Patent Citations (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1326429A (en) * | 1969-10-31 | 1973-08-15 | Siemens Ag | Production of high-velocity gas jets |
| WO2011156413A2 (en) * | 2010-06-07 | 2011-12-15 | University Of Florida Research Foundation, Inc. | Dielectric barrier discharge wind tunnel |
| CN103175672A (en) * | 2013-02-28 | 2013-06-26 | 山东大学 | Construction machinery radiator air tunnel capable of simulating wind and sand impact and using method thereof |
| CN104251767A (en) * | 2013-06-28 | 2014-12-31 | 中国科学院工程热物理研究所 | Gas flow field measurement system based on alternating-current discharge plasma sensors |
| CN105836165A (en) * | 2016-05-05 | 2016-08-10 | 哈尔滨工业大学 | Space environment ground-based simulation plasma generating device and plasma generating method achieved through device |
| CN207623147U (en) * | 2017-12-27 | 2018-07-17 | 天津亭华科技有限公司 | A kind of sand dust test chamber |
| CN109470504A (en) * | 2018-12-13 | 2019-03-15 | 中国航天空气动力技术研究院 | A kind of phase shift device and method for electro-arc heater arc root rotation of strengthening communication |
| CN110082058A (en) * | 2019-04-22 | 2019-08-02 | 南京航空航天大学 | A kind of multi-fan array wind-tunnel that simulating a variety of extreme wind fields and simulation of wind method |
| CN110933832A (en) * | 2019-07-16 | 2020-03-27 | 中国人民解放军空军工程大学 | Single power supply driven array type plasma synthetic jet flow control device and flow control method |
| JP2021047086A (en) * | 2019-09-18 | 2021-03-25 | 株式会社Ｓｕｂａｒｕ | Wind tunnel test apparatus |
| CN110763966A (en) * | 2019-11-21 | 2020-02-07 | 华北电力大学（保定） | Sand and dust weather simulation experiment system |
| CN211264574U (en) * | 2020-02-03 | 2020-08-14 | 海南泰和鸿鼎实业有限公司 | Sand storm simulator |
| CN111577561A (en) * | 2020-04-24 | 2020-08-25 | 南京理工大学 | Device for improving jet intensity of annular electrode exciter and working method thereof |
| CN112067237A (en) * | 2020-09-24 | 2020-12-11 | 北京卫星环境工程研究所 | Hypersonic wind tunnel based on plasma |
| CN112135408A (en) * | 2020-09-24 | 2020-12-25 | 北京卫星环境工程研究所 | Plasma parameter measuring method for plasma wind tunnel |
| CN112399694A (en) * | 2020-11-04 | 2021-02-23 | 中国空气动力研究与发展中心低速空气动力研究所 | Annular plasma exciter and pneumatic excitation generating method thereof |
Non-Patent Citations (4)
| Title |
|---|
| ZHAO ZIJIE: "Plasma flow control over forebody at high angles of attack" * |
| 王靖宇: "基于等离子体流动控制的方背式汽车模型减阻研究" * |
| 车学科;聂万胜;侯志勇;何浩波;田希晖;田学敏;: "地面试验模拟高空等离子体流动控制效果" * |
| 阳鹏宇: "磁加速等离子体激励器激励特性" * |
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